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Apollo 14 composite casting demonstrationThe purpose of the demonstration was to show that mixtures of materials of different specific gravities would remain stable in the liquid state and during freezing in low g and not segregate as they do on earth. An inflight demonstration was performed on the Apollo 14 mission during the translunar and and transearth coast periods. The apparatus consisted of an electrical heater, a heat sink device for cooling, and sealed metal capsules containing matrix materials having a low-melting point and dispersants. The evaluation of the demonstration samples was accomplished by comparing space processed (flight) samples with (control) samples processed on the ground under otherwise similar conditions. In the low q environment of space flight the dispersions of particles, fibers, and gases in a liquid metal matrix were maintained during solidification. Dispersions of normally immiscible liquids were also maintained during solidification.
Document ID
19720015848
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Yates, I. C., Jr.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-TM-X-64641
Report Number: NASA-TM-X-64641
Accession Number
72N23498
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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